As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NOSE WHEEL WELL TOP PANEL WEB FOUND WITH A CRACK AT BS 310 AT LBL 10. CRACK LENGTH IS 1.125 INCHES. INTERIM REPAIR ACCOMPLISHED IAW SRM 53-10-04, FIG 116. SHEETS 1 AND 6 AND FIG 117 SHEETS 1 THRU 10. REQUIRES INITIAL INTERNAL DETAIL VISUAL INSPECTION PRIOR TO 15,000 FC. (K)